4.6 Article

Autonomous Trajectory Optimisation for Intelligent Satellite Systems and Space Traffic Management

期刊

ACTA ASTRONAUTICA
卷 194, 期 -, 页码 185-201

出版社

PERGAMON-ELSEVIER SCIENCE LTD
DOI: 10.1016/j.actaastro.2022.01.027

关键词

Distributed space systems; Intelligent satellite systems; Avionics; Astrionics; Artificial intelligence; Collision avoidance; Trajectory optimisation; Optimal control; SmartSat

向作者/读者索取更多资源

Recent advances in AI, sensing, and computing technologies have led to the development of new concepts for the safe and efficient operation of Distributed Space Systems in near-Earth orbits. These technologies enable higher levels of autonomy in small satellite constellations, facilitating a more responsive and resilient approach to Space-Based Space Surveillance.
Recent advances in Artificial Intelligence (AI), sensing and computing technologies have led to the development of new promising concepts for the safe and efficient operation of Distributed Space Systems (DSS) in near-Earth orbits. The combined use of these technologies allows higher levels of autonomy in small satellite constellations or clusters, facilitating a more responsive and resilient approach to Space-Based Space Surveillance (SBSS), both in terms of data collection and data processing. This article presents an innovative DSS mission management approach exploiting multiple heterogeneous space platforms capable of autonomously calculating attitude and orbit raising manoeuvres to maximise mission efficiency and minimise the risk of collision with resident space objects. Furthermore, it addresses the development of reactive mission planning capabilities and lays foundations for introducing predictive system functionalities, by adopting heuristic multiple-direct-shooting trajectory optimisation algorithms based on the particle swarm technique. These functionalities provide DSS with higher levels of autonomy and support the introduction of new mission concepts while mitigating the threats of the space environment. The first verification case study addresses the problem of an orbit raising manoeuvre for debris collision avoidance, where the thrust activation and vectoring angle profiles are optimised to achieve the orbital semi-major axis increment which reduces the probability of collision to an acceptable level. An inverse dynamic method is employed in the second case study, which addresses an optimal attitude reorientation problem for initial debris tracking. Typical attitude constraints and forbidden pointing zones are considered, highlighting the suitability and general applicability of the proposed DSS functionalities for the intended SBSS mission.

作者

我是这篇论文的作者
点击您的名字以认领此论文并将其添加到您的个人资料中。

评论

主要评分

4.6
评分不足

次要评分

新颖性
-
重要性
-
科学严谨性
-
评价这篇论文

推荐

暂无数据
暂无数据